View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 04384U 70036B 22268.81320052 -.00000021 00000-0 -42479-4 0 9991
2 04384 74.0310 28.2045 0053099 147.3546 329.9364 12.39223518371208
| Epoch (UTC): | 25 September 2022 19:31:00 |
| Eccentricity: | 0.0053099 |
| inclination: | 74.0310° |
| perigee height: | 1468 km |
| apogee height: | 1552 km |
| right ascension of ascending node: | 28.2045° |
| argument of perigee: | 147.3546° |
| revolutions per day: | 12.39223518 |
| mean anomaly at epoch: | 329.9364° |
| orbit number at epoch: | 37120 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|